Service difficulty reports

1,771,708 reports of malfunctions and defects, newest first. Air carriers must report; general aviation reporting is voluntary.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SWAA2026021789417Data Plate · missingMISSING ENGINE DATA PLATE.Feb 17, 2026 · N7728D · Boeing 7377BD · Engine (Turbine/Turboprop)SDR SWIA2026021677399Skin · dentedBS 169-173 SMALL DENT LESS THAN 1 DIAMETER DEPT OF 010 PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. REMOVED AND REPLACED SKINS PER SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-Feb 16, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR DALA2026082204777Skin · not reportedFUSELAGE SKIN, FR 34, BETWEEN S1R AND S1L, PCS TIMING DOUBLER AREA, INSTALLATION DEVIATION, INCORPORATION OF SECTION II SUPPLEMENTAL INSPECTIONS. REVISION B OF ER/A 554177-14 INCORPORATES SECTION II SUPPLEMENTAL INSPECTIONS. INSPECTIONS THRESHOLD IS 33,481Feb 16, 2026 · N301NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR REXA2026080301394Fitting · corrodedCORROSION ON MACHINED FITTING LOCATED ON FS847 BETWEEN STRG 25L TO STRG 25R (INTERNAL FUSELAGE). MACHINED FITTING LOCATED ON FS847 BETWEEN STRG 25L TO STRG 25R (INTERNAL FUSELAGE) WERE REPAIRED PER REO 670-53-41-834 REV --Feb 16, 2026 · N398CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR REXA2026080301393Fitting · corrodedCORROSION ON MACHINED FITTING LOCATED ON FS847 BETWEEN STRG 25L TO STRG 25R (INTERNAL FUSELAGE). MACHINED FITTING LOCATED ON FS847 BETWEEN STRG 25L TO STRG 25R (INTERNAL FUSELAGE) WERE REPAIRED PER REO 670-53-41-834 REV --Feb 16, 2026 · N398CA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2026021676178Skin · gougedTECH HIT AIRCRAFT WITH MAN LIFT ON RT SKIN PANEL AND DENT AND GOUGED SKIN FROM FS 1108 TO FS 1126 BETWEEN STRG 16R AND STRG 18R. REPAIRED SKIN DAMAGE FROM FS1108 TO FS1126 IAW REO 670-53-61-2684 REV -Feb 16, 2026 · N716SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2026021675983Intercostal · corrodedINTERCOSTAL LEFT OF STRINGER 27 BETWEEN FS 349.00 AND 379.00 IS CORRODED. REMOVED AND REPLACED THE INTERCOSTAL LEFT OF STGR 27 BETWEEN FS349 - FS364, NEW SERVICEABLE L/H INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND SRM51-42-21-001-001-A01.Feb 16, 2026 · N795SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2026021675846Cleat · corrodedFOUND CORROSION ON PASSENGER DOOR DD4 MID INTERCOSTAL AND FS335.163 CLEAT. PAX DOOR DD4 FS335.163 CLEAT, ORIGINAL MATERIAL THICKNESS IS 0.050" IAW SRM 52-10-14-00 CORROSION ON MORE THAN ONE ELEMENT AT A GIVEN CROSS-SECTION, PAX DOOR DD4 FS335.163 INBD CLEAT Feb 16, 2026 · N959SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026021675842Skin · gougedRH WING INBOARD FLAP UPPER INTERNAL SKIN HAS MULTIPLE GOUGES UNDER PANEL 684AB. REMOVED MULTIPLE GOUGES AND RESTORED AREA AT RH WING INBOARD FLAP UPPER INTERNAL SKIN UNDER PANEL 684AB REF SRM 51-12-00, COMPLIED WITH ALL THE STEPS OF THE REO 601R-57-52-2543 REFeb 16, 2026 · N959SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2026021675634Stringer Splice · not reportedFABRICATION REQUIRED FOR STRINGER 26R, SPLICE, AFT OF FRAME STATION 969 PN BA670-35119-2. COMPLIED WITH SNIEO BA670-35119.Feb 16, 2026 · N631SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SIMA20260216003Sign · cracked251HLW AND 252HRW EMERGENCY EXIT LIGHT CRACKED. R & R 251HLW AND 252HRW EMERGENCY EXIT LIGHT IAW EMBRAER ERJ 175 AMM 33-50-15. OP CHECKS GOOD.Feb 16, 2026 · N205NN · Emb ERJ170200LR · Emergency LightingSDR SIMA20260216004Light · damagedEMERGENCY PHOTO LUMINESCENT LIGHT STRIPS RT NR 1, 3, 4, &12, LT NR 1 ARE DAMAGED. R & R EMERGENCY PHOTOLUMINESCENT LIGHT STRIPS RT NR 1, 3, 4, & 12, LT NR 1 IAW AMM 33-50-21 OPS CKD GOOD.Feb 16, 2026 · N205NN · Emb ERJ170200LR · Emergency LightingSDR SWAA2026032371185Bear Strap · crackedCRACKED BEAR STRAP AT SERVICE DOOR CUT OUT. BS 294.5, BTWN STRINGERS 8 - 9R. PERFORMED A CATEGORY B REPAIR ON THE BEAR STRAP BS 277 - 320, S6 - 11R. IAW SRM 53-10-01R-6, REPAIR 6, EA 26-153-00560-WIP1, EA 26-153-00560-WIP2, & EA 26-153-00560.Feb 16, 2026 · N245WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2026032371373Rub Strip · wornWORN RUB STRIP, BODY FAIRING BS 540 + 10. RBL 41. REPAIRED IAW SRM 57-10-13-2R-3, REPAIR 3, & SRM 51-40-02.Feb 16, 2026 · N7889A · Boeing 73779L · Fuselage Miscellaneous StructureSDR SWAA2026032371187Stub Frame · crackedCRACK INDICATION ON STUB FRAME, BS 294.5 - 296.5, BTWN STRINGER 8 - 9R. REPLACED THE STUB FRAME IAW SRM 51-10-02, & DWG 141A8370, SHEET 1, REV C.Feb 16, 2026 · N245WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2026032371280Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 661BB AT RT WING T/E. REPAIRED THE ACCESS PANEL 661BB IAW SRM 51-70-04-2R-10, REPAIR 10 .Feb 16, 2026 · N245WN · Boeing 7377H4 · Wing, Plate/SkinSDR SWAA2026032371282Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 561BB AT LT WING. REPAIRED ACCESS PANEL 561BB AT LT WING IAW SRM 51-70-04-2R-10 REPAIR 10.Feb 16, 2026 · N7889A · Boeing 73779L · Wing, Plate/SkinSDR SWAA2026032371375Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 661BB AT RT WING. REPAIRED THE ACCESS PANEL 661BB AT RT WING IAW SRM 51-70-04-2R-10 REPAIR 10.Feb 16, 2026 · N7889A · Boeing 73779L · Wing, Plate/SkinSDR SWAA2026031871163Seat Back · out of adjustPERFORMED ADJUSTMENT ON SEAT ROW 14B FOR RECLINING AT EMERGENCY EXIT AREA AT PASSENGER CABIN. VERIFIED ADJUSTMENT OF PASSENGER SEAT 14B RECLINE IS NOT NECCESSARY. WAS LEFT LOCKED IAW REV.6, CMM 25-21-45 TABLE 1 AND DRAWING DG306-142007C, STEP 6, PAGE 8006.Feb 16, 2026 · N463WN · Boeing 7377H4 · Passenger Compartment EquipmentSDR HNAA2026031800226Angle · crackedRIGHT OVERWING FAIRING 1ST ANGLE CRACKED. REPAIRED ANGLE IAW SRM 57-20-01REFeb 16, 2026 · N644AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026031700217Angle · crackedLT OVERWING FAIRING 1ST ANGLE CRACKED. REMOVED, FABRICATED ANGLE, AND INSTALLED IAW SRM 57-20-01Feb 16, 2026 · N644AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026031100207Angle · crackedLEFT OVERWING FAIRING 4TH ANGLE CRACKED. REPAIRED ANGLE IAW SRM 57-20-01 ITEM 3 (FIG 205)Feb 16, 2026 · N644AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR 2026FA0000165Alternator · failedPILOT HAD AN ALTERNATOR FAILURE IN CRUISE.Feb 16, 2026 · N6149K · Cessna R172K · AC Generator-AlternatorSDR SWIA2026021675428Flap Track · wornRT WING FLAP TRACK OUTBD 2A HAS A WIDTH REDUCTION OF .37MM THE WHOLE LENGTH. I.D.# TC2-10393 CAL DUE: 6-17-26. (C-CHECK RO 03/05/2026)REMOVED AND REPLACED RH WING FLAP TRACK OUTBD 2A REF EMB 175 AMM 57-54-25. ASSET #HG2-50002 CAL DUE 9/18/26. OPS AND GAP CHEFeb 16, 2026 · N140SY · Emb ERJ170200LR · Trailing Edge FlapsSDR HNAA2026030400196Angle · crackedRIGHT OVERWING FAIRING 4TH ANGLE CRACKED. R A R ANGLE IAW SRM 51-40-02Feb 16, 2026 · N644AE · Emb EMB145LR · Aerodynamic FairingsSDR DALA2026030401478Fan · faultedVENT AVIONICS SYS FAULT DISPLAYED. WARM ELECTRICAL ODOR IS PRESENT. R & R AEVC IAW AMM 21-26. STILL REQ OPS CHK. OPS TEST OF AEVC FAULTED 21-26-51 EXTRACT FAN 18HQ AND 21-26-55 ISOLATION VALVE 24HQ. R & R EXTRACT FAN 18HQ IAW AMM 21-26. AEVC TESTED GOOD,Feb 16, 2026 · N353NB · Airbus A319114 · Air Distribution FanSDR SWAA2026030371345Support Angle · crackedCRACKED SUPPORT ANGLE, BS 907 - 927, S25R - S27R. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 147A7221, SHEET 24, REV - .Feb 16, 2026 · N7731A · Boeing 73776N · Fuselage Miscellaneous StructureSDR HNAA2026030200164Angle · crackedRIGHT OVERWING FAIRING 5TH ANGLE CRACKED. CUTOUT PERFORMED, REPAIR DOUBLER AND FILLER INSTALLED IAW SRM 57-20-01 AND EO1-57-26-0079Feb 16, 2026 · N644AE · Emb EMB145LR · Aerodynamic FairingsSDR JIKA2026030201Landing Gear · faultedTHE FLIGHT CREW REPORTED THAT WHEN THE LANDING GEAR HANDLE WAS ACTUATED TO THE DOWN POSITION THE GEAR DID NOT EXTEND NORMALLY AND THEY RECEIVED NO GREEN SAFE LIGHTS. THE AMBER HANDLE LIGHT WAS ILLUMINATED, AND THE HYDRAULIC PUMP COULD BE HEARD RUNNING CONTINUOFeb 16, 2026 · N968AF · Saab 340B · Landing Gear Retraction/Extension SystemSDR 2026F00018Pressure Switch · failedWING ANTI-ICE CAS MESSAGE "WNG A/I FAIL" WING ANTI-ICE INDICATED FAILED IN FLIGHT. SYSTEM WAS NOT IN USE AND NOT NEEDED FOR THE CONDITIONS WHEN THE INDICATION HAPPENED. CREW ELECTED TO DIVERT TO HOME BASE AIRPORT AS THEY WERE IN THE VACINITY FOR MAINTENANCE SUFeb 16, 2026 · N92DJ · Emb EMB505 · Airfoil Anti/De-ice SystemSDR SWAA2026022771167Bracket · crackedSUPPORT STANDOFF FWD OF AE0104A DISCONNECT BRACKET IS CRACKED. REMOVED AND REPLACED SUPPORT STANDOFF FWD OF AE0104A DISCONNECT BRACKET (NUTSPACE) IAW SRM 51-40-02-0G-0 AND AIPC 25-50-51-45A DETAIL F.Feb 16, 2026 · N247WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWIA2026022575290Windshield · crackedWINDSHIELD CRACKED ENROUTE. RAN QRH. NO PRESSURIZATION ISSUES. (FLIGHT 6394 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 31750315. REMOVED AND REPLACED LH CA WINDSHIELD IAW TASK CARD 56-220-1000-SKY AND REFERENCING APPLICABLE STEPS OF AMM 56Feb 16, 2026 · N709SK · Cndair CL6002C10 · Flight Compartment WindowsSDR SWAA2026022471406Fairing · crackedRIGHT WING T/E PANEL 651FB INBD END LOWER CLOSEOUT FAIRING IS CRACKED. REMOVED AND REPLACED RIGHT WING T/E PANEL 651FB INBD IAW DWG 115A2200, AND AMM 20-50-11-910-801, TABLE 204.Feb 16, 2026 · N8794Q · Boeing 7378 · Trailing Edge FlapsSDR SIMA20260216002Shear Tie · corrodedAFT GALLEY UNDERFLOOR CENTER SHEAR CLIP AFT OF AFT DRAIN MAST ON FR 87 IS CORRODED. (LEVEL 2 CORROSION). REMOVED AND REPLACED AFT GALLEY UNDERFLOOR CENTER SHEAR CLIP AFT OF AFT DRAIN MAST ON FR 87 IAW SRM 51-40-08.Feb 16, 2026 · N770JM · Emb ERJ170100LR · Fuselage Internal Mounting StructureSDR HNAA2026022400156Angle · crackedRIGHT OVERWING FAIRING 2ND ANGLE CRACKED. RAR ANGLE IAW SRM 51-40-02Feb 16, 2026 · N644AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR AALA202602232228Hinge Arm · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM #1 ELEVATOR ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ARM #1 ELEVATOR ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Feb 16, 2026 · N8009T · Airbus A319115 · Elevator StructureSDR AALA202602228791Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON LH CONTINUITY FITTING ON WINDSHIELD LOWER ATTACHMENT AREA L: 0.157 IN. MAINTENANCE REPLACED LH CONTINUITY FITTING OF THE WINDSHIELD CENTER POST LOWER ATTACHMENT INTERNAL AREA IAW EA 370750 AND A319 SRM 51Feb 16, 2026 · N829AW · Airbus A319132 · Fuselage Main, StructureSDR AALA202602224401Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON RH CONTINUITY FITTING ON WINDSHIELD LOWER ATTACHMENT AREA L: 0.157 IN. MAINTENANCE REPLACED RH CONTINUITY FITTING OF THE WINDSHIELD CENTER POST LOWER ATTACHMENT INTERNAL AREA IAW EA 370750 AND A319 SRM 5Feb 16, 2026 · N829AW · Airbus A319132 · Fuselage Main, StructureSDR AALA202602202970Coffeemaker · overheatedAIRCRAFT WAS NOT GROUNDED: AFT GALLEY COFFEE POTS HAVE ELECTRICAL BURNING SMELL. TURNED OFF AND SMELL WENT AWAY. ACCOMPLISHED JOB CARD 26L00021001 SMOKE ODER FUME INITIAL TROUBLESHOOTING DETERMINED AFTER LEFT COFFEE MAKER INOP CAUSEOF ELECTRICAL SMELL PLACED OFeb 16, 2026 · N745VJ · Airbus A319112 · Buffet/GalleysSDR AALA202602206711Proximity Sensor · faultyAIRCRAFT WAS NOT GROUNDED: DOOR AFT CARGO ECAM AFTER TAKEOFF CLIMBING THROUGH 12K. INTERRUPTED BACK TO MID ACCOUNT MAINTENANCE, CARGO DOOR LIGHT. FLIGHT DID NOT DECLARE AN EMERGENCY AND WAS NOT OVERWEIGHT FOR LANDING. MAINTENANCE AFT CARGO DOOR PROX SWITCH OPSFeb 16, 2026 · N9002U · Airbus A319115 · Door Warning SystemSDR SWAA2026022071277Handle · crackedFED UPPER DOOR ASSIST HANDLE IS CRACKED. REMOVED AND REPLACED FED UPPER DOOR ASSIST HANDLE IAW AMM 52-11-31-000-802 STEPS 2. F. (3) AND AMM 52-11-31-400-802 STEPS 3. G. (2).Feb 16, 2026 · N8683D · Boeing 7378H4 · Passenger/Crew DoorsSDR HNAA2026022000144Fairing · crackedLEFT OVERWING FAIRING CRACKED AT 2ND ANGLE. RAR ANGLE IAW SRM 51-40-02Feb 16, 2026 · N644AE · Emb EMB145LR · Aerodynamic FairingsSDR DALA2026021901222Oxygen Mask · unwanted deployAFT GALLEY CREW OXYGEN MASKS DEPLOYED. OXYGEN NOT DISCHARGED. REINSTALLED MASKS IAW AMM 35-21. (LP: 7363468)Feb 16, 2026 · N340NW · Airbus A320212 · Passenger Oxygen SystemSDR DALA2026021901221Skin · corrodedON WALKAROUND FOUND CORROSION ON AFT FUSELAGE AROUND LAV VENT OVERBAORD. REF LOG# 1453283 FOR CORRECTIVE ACTION PERFORMED. (LP: 8279240)Feb 16, 2026 · N345NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2026021901220Skin · corrodedFUSELAGE SKIN CORRODED AROUND LAV VENT. REPAIRED CORROSION PER A320, SRM 53-41-11-300-004. (LP: 1453283)Feb 16, 2026 · N345NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2026021901219Structure · damagedUNREPAIRED EXISTING HOLES DIAMETER EQUAL TO OR GREATER THAN MINIMUM STARTING HOLE DIAMETER WAS FOUND. ON HOLES H1: 0.2634 IN , H2: 0.3321IN, H7: 0.2017 IN, H8: 0.2920 IN, HA:0.2027 IN, HB: 0.2620 IN, HC: 0.2030 IN, HD : 0.2631 IN, H9: 0.2032 IN, H10: 0.2631 INFeb 16, 2026 · N362NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2026021901215Oxygen Bottle · damagedOXYGEN CONTAINER AT ROW 28ABC FOUND DAMAGED. REMOVED AND REPLACED OXYGEN CONTAINER AT ROW 28ABC IAW AMM 35- 21-41-000-001-A AND 35-21-41-400-001-A. PERFORMED SATISFACTORY OP CHK OF MANUAL MASK RELEASE IAW AMM 35-23-00-710-001-A. JOB COMPLETE. (LP: 1453153)Feb 16, 2026 · N358NB · Airbus A319114 · Passenger Oxygen SystemSDR SWAA2026021972185Seal · out of adjustCREW REPORTS LT HORIZONTAL STAB FWD LOWER SLIDE SEAL NOT FLUSH. REMOVED LT STAB FWD LOWER SLIDER. OK TO CONTINUE PER CDL 55-10-1 SP1B. INSTALLED SEAL I/A/W 53-31-31 STEPS F 1 THRU 5. REPLACED LT HORIZONTAL STAB SLIDE SEAL IAW AMM 53-31-31. THIS CLEARS MEL.Feb 16, 2026 · N462WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2026021971612Hmu · failedNR 2 ENG SLOW TO ACCELARATE WOULD NOT GO ABOVE 83.5%. NR 1 ENG WAS AT REQ. N1 OF 91.3% REJECTED TAKEOFF AT APPROX 75 KNOTS. REMOVED AND REPLACED NR 2 ENGINE HMU, FUEL PUMP ASSY IAW TTG8Q01AG805; MT 773-11-00. COMPLIED WITH THE INSPECTION REQUIREMENTS OF THISFeb 16, 2026 · N8303R · Boeing 7378H4 · Fuel Controlling SystemSDR GTIA2026021939281Ecs · contaminatedAFTER LANDING FUMES SMELL FROM THE AFT OF AIRCRAFT POSSIBLY FROM PACK 2. FA STATES THAT THE SMELL CAME AROUND THE TIME THE GEAR CAME DOWN ON APPR. APU WAS OFF DURING THAT TIME.-REF TSM 05-50-00-810-831-A. ACCOMPLISHED LEVEL A DECONTAMINATION PROCEDURE AND R+R Feb 16, 2026 · N652NK · Airbus A320232 · Cabin Cooling System